N50105

Substantial
None

MOONEY M20J S/N: 24-3059

Accident Details

Date
Thursday, May 26, 1994
NTSB Number
FTW94LA181
Location
WILLCOX, AZ
Event ID
20001206X01304
Coordinates
32.430141, -109.880523
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

THE FAILURE OF THE CONNECTING ROD DUE TO LACK OF LUBRICATION. FACTORS WERE THE PREVIOUS DAMAGE TO THE ENGINE, AND THE UNSUITABLE TERRAIN AT THE PILOT'S DISPOSAL FOR THE FORCED LANDING.

Aircraft Information

Registration
N50105
Make
MOONEY
Serial Number
24-3059
Engine Type
Reciprocating
Year Built
1944
Model / ICAO
M20J M20P
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
FELL RICHARD
Address
4513 N CLARK ST
Status
Deregistered
City
CHICAGO
State / Zip Code
IL 00000
Country
United States

Analysis

On May 25, 1994, at 1800 Pacific daylight time, a Mooney M20J, N50105, was substantially damaged during a forced landing near Willcox, Arizona. The instrument rated private pilot was not injured. Visual meteorological conditions prevailed for the business flight.

An IFR flight plan was filed for a flight from Fort Stockton, Texas, to Scottsdale, Arizona. The pilot reported that he was in cruise flight at an assigned altitude of 10,000 feet, when "he noticed a change in engine and propeller sound, accompanied by the propeller RPM increasing beyond the red line." Propeller control could not be regained by moving the propeller control lever, and "when the power was reduced, the engine began to shake violently." When the pilot closed the throttle, the engine stopped.

After declaring an emergency, and establishing a glide to the Cochise County Airport, near Willcox, Arizona, the pilot attempted to restart the engine with the starter without success.

The pilot further stated that the airport was beyond the gliding distance of the airplane, and a forced landing was attempted on the rough and uneven desert, "pretty well covered by mesquite and brush." The right main landing gear was torn from the wing during the landing roll. Both wings and horizontal stabilizers sustained substantial damage due to a collision with mesquite trees and a fence.

A detailed examination of the 580 hour engine revealed that the 3 and 4 connecting rods had failed due to lack of lubrication. A bearing was found to have spun, blocking the oil flow.

According to the aircraft and engine records, an incident involving the operation of the engine with low oil occurred approximately 108 hours prior to the accident. The details of the incident are enclosed in the pilot/operator report.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94LA181